PREDICTION OF SECONDARY FLOW FEATURES IN A LOW PRESSURE TURBINE

被引：0

作者：

Jonak, Pawel ^{[1
]}

Borzecki, Tomasz ^{[2
]}

Konopa, Maciej ^{[3
]}

Kubacki, Slawomir ^{[1
]}

机构：

[1] Warsaw Univ Technol, Inst Aeronaut & Appl Mech, Nowowiejska 24, PL-00665 Warsaw, Poland

[2] Avio Aero, Grazynskiego 141, PL-43300 Bielsko Biala, Poland

[3] Polonia Aero Sp Zoo, Lab Badan Napedow Lotniczych, 111 Eskadry Mysliwskiej 1, PL-05220 Zielonka, Poland

来源：

PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2018, VOL 2B | 2018年

关键词：

ENDWALL;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A simulation of the flow through a four-stage low pressure turbine (LPT) of an aero-engine is performed using an eddy viscosity based RANS model. An analysis of secondary flow details in the vicinity of endwalls and strut surface is performed. An interaction of wakes generated by the swirler vanes and end wall boundary layers is also studied. The CFD results are compared with own test rig data of LPT obtained in Polonia Aero Lab in Zielonka (Poland). Global flow parameters were reproduced in good agreement with experiment (difference less than 1.5%). Satisfactory agreement between measured and predicted pressure distribution on the surface of inlet strut has been obtained.

引用

页数：12

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